Date:
May 10th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5812 51 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2007/124/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2103763
29 A = 6715125
04 meter
Y = -4971560
20 meter E =
0016447
Z = -4012371
13 I = 51
46634
XDOT = 6625
729126 Wp = 129
80581
YDOT = -337
403525 meter/sec RA = 329
23003 deg
ZDOT = 3892
245354 TA = 180
50099
MA = 180
50264
Ha = 187
829 n
mi
Hp = 175
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6902110
52 X = 2178691
38
Y = -16310893
05 feet Y = -4947615
43 meter
Z = -13163947
27 Z = -4001969
31
XDOT = 21737
956451 XDOT = 6610
101394
YDOT = -1106
966946 feet/sec YDOT = -263
398652 meter/sec
ZDOT = 12769
833838 ZDOT = 3924
395776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2108369
12 X = -642630
91
Y = -17614026
80 feet Y = -5368755
37 meter
Z = -13125346
06 Z = -4000605
48
XDOT = 16929
786968 XDOT = 5160
199068
YDOT = -11631
839656 feet/sec YDOT = -3545
384727 meter/sec
ZDOT = 12890
884295 ZDOT = 3929
141533
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07124
47746049
00020000 00000-0 20000-3 0 9004
2 25544 51
6338 329
7276 0010167 145
3643 214
8186 15
77549773 3878
Satellite: ISS
Catalog Number: 25544
Epoch time: 07124
47746049 = yrday
fracday
Element set: 900
Inclination: 51
6338 deg
RA of node: 329
7276 deg
Eccentricity:
0010167
Arg of perigee: 145
3643 deg
Mean anomaly: 214
8186 deg
Mean motion: 15
77549773 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 387
Checksum: 314
Coasting Arc #2 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2007/125/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5208195
80 A = 6714136
05 meter
Y = -390180
17 meter E =
0014288
Z = -4226955
17 I = 51
43841
XDOT = 3339
588631 Wp = 113
16827
YDOT = -5941
541300 meter/sec RA = 324
10441 deg
ZDOT = -3581
481332 TA = 120
39830
MA = 120
25700
Ha = 187
632 n
mi
Hp = 175
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17087256
55 X = -5182911
55
Y = -1280118
66 feet Y = -448279
30 meter
Z = -13867963
14 Z = -4252195
61
XDOT = 10956
655612 XDOT = 3423
178065
YDOT = -19493
245735 feet/sec YDOT = -5903
728387 meter/sec
ZDOT = -11750
266836 ZDOT = -3565
054956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15243952
81 X = -4646356
82
Y = 7654269
21 feet Y = 2333021
26 meter
Z = -13963076
57 Z = -4255945
74
XDOT = -20
424647 XDOT = -6
225432
YDOT = -21274
422419 feet/sec YDOT = -6484
443953 meter/sec
ZDOT = -11689
082484 ZDOT = -3562
832341
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07125
49099870
00020000 00000-0 20000-3 0 9011
2 25544 51
6329 324
4939 0010091 149
5251 210
6503 15
77568262 4033
Satellite: ISS
Catalog Number: 25544
Epoch time: 07125
49099870 = yrday
fracday
Element set: 901
Inclination: 51
6329 deg
RA of node: 324
4939 deg
Eccentricity:
0010091
Arg of perigee: 149
5251 deg
Mean anomaly: 210
6503 deg
Mean motion: 15
77568262 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 403
Checksum: 286
Coasting Arc #3 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2007/126/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3553859
22 A = 6719986
25 meter
Y = 5296382
27 meter E =
0022455
Z = 2073480
48 I = 51
43688
XDOT = -5208
676322 Wp = 127
71366
YDOT = -1315
666057 meter/sec RA = 318
88245 deg
ZDOT = -5539
674838 TA = 28
99622
MA = 28
87167
Ha = 187
434 n
mi
Hp = 175
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11659643
12 X = -3622892
72
Y = 17376582
26 feet Y = 5256254
80 meter
Z = 6802757
47 Z = 2056048
56
XDOT = -17088
833079 XDOT = -5166
666180
YDOT = -4316
489688 feet/sec YDOT = -1373
676854 meter/sec
ZDOT = -18174
786213 ZDOT = -5564
876997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -729609
30 X = -222384
91
Y = 20934215
13 feet Y = 6380748
77 meter
Z = 6737707
72 Z = 2053653
31
XDOT = -15171
259844 XDOT = -4624
200000
YDOT = 5380
336810 feet/sec YDOT = 1639
926660 meter/sec
ZDOT = -18269
867346 ZDOT = -5568
655567
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07126
50451391
00020000 00000-0 20000-3 0 9025
2 25544 51
6336 319
2602 0009893 153
1448 207
0230 15
77646387 4196
Satellite: ISS
Catalog Number: 25544
Epoch time: 07126
50451391 = yrday
fracday
Element set: 902
Inclination: 51
6336 deg
RA of node: 319
2602 deg
Eccentricity:
0009893
Arg of perigee: 153
1448 deg
Mean anomaly: 207
0230 deg
Mean motion: 15
77646387 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 419
Checksum: 283
Coasting Arc #4 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2007/127/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3798528
32 A = 6710194
54 meter
Y = 1988886
00 meter E =
0013257
Z = 5157242
35 I = 51
38164
XDOT = -4635
057651 Wp = 147
67199
YDOT = 6070
704785 meter/sec RA = 313
72982 deg
ZDOT = 1060
445868 TA = 292
12017
MA = 292
26085
Ha = 187
360 n
mi
Hp = 176
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12462363
26 X = 3750952
86
Y = 6525216
54 feet Y = 2031096
67 meter
Z = 16920086
45 Z = 5175580
41
XDOT = -15206
882057 XDOT = -4707
748156
YDOT = 19917
010450 feet/sec YDOT = 6018
466420 meter/sec
ZDOT = 3479
153111 ZDOT = 1037
752722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13927696
02 X = 4245161
75
Y = -1248204
34 feet Y = -380452
68 meter
Z = 16989395
04 Z = 5178367
61
XDOT = -2040
630201 XDOT = -621
984085
YDOT = 23978
742342 feet/sec YDOT = 7308
720666 meter/sec
ZDOT = 3394
372570 ZDOT = 1034
604759
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07127
51800984
00020000 00000-0 20000-3 0 9034
2 25544 51
6325 314
0258 0010029 156
9563 203
2054 15
77607098 4352
Satellite: ISS
Catalog Number: 25544
Epoch time: 07127
51800984 = yrday
fracday
Element set: 903
Inclination: 51
6325 deg
RA of node: 314
0258 deg
Eccentricity:
0010029
Arg of perigee: 156
9563 deg
Mean anomaly: 203
2054 deg
Mean motion: 15
77607098 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 435
Checksum: 278
Coasting Arc #5 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2007/128/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4366293
09 A = 6721703
77 meter
Y = -5101975
78 meter E =
0012858
Z = 295888
67 I = 51
40125
XDOT = 3474
932384 Wp = 93
75655
YDOT = 3335
357459 meter/sec RA = 308
54139 deg
ZDOT = 6008
291246 TA = 269
47231
MA = 269
61965
Ha = 187
245 n
mi
Hp = 176
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14325108
55 X = 4421582
23
Y = -16738765
67 feet Y = -5052840
34 meter
Z = 970763
34 Z = 317233
97
XDOT = 11400
696798 XDOT = 3408
190366
YDOT = 10942
773814 feet/sec YDOT = 3373
842298 meter/sec
ZDOT = 19712
241622 ZDOT = 6025
010766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2540775
38 X = 774428
34
Y = -21880999
43 feet Y = -6669328
63 meter
Z = 1050579
37 Z = 320216
59
XDOT = 13879
993359 XDOT = 4230
621976
YDOT = 2593
948454 feet/sec YDOT = 790
635489 meter/sec
ZDOT = 19775
615228 ZDOT = 6027
607521
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07128
53148039
00020000 00000-0 20000-3 0 9044
2 25544 51
6316 308
7909 0009982 161
5237 198
6292 15
77672777 4516
Satellite: ISS
Catalog Number: 25544
Epoch time: 07128
53148039 = yrday
fracday
Element set: 904
Inclination: 51
6316 deg
RA of node: 308
7909 deg
Eccentricity:
0009982
Arg of perigee: 161
5237 deg
Mean anomaly: 198
6292 deg
Mean motion: 15
77672777 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 451
Checksum: 322
Coasting Arc #6 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2007/129/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2272906
77 A = 6710605
07 meter
Y = -3851077
71 meter E =
0020244
Z = -5020410
57 I = 51
34666
XDOT = 5215
729757 Wp = 128
98029
YDOT = -5375
395766 meter/sec RA = 303
33947 deg
ZDOT = 1754
233973 TA = 158
04148
MA = 157
95461
Ha = 187
103 n
mi
Hp = 176
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7457043
20 X = -2205286
24
Y = -12634769
37 feet Y = -3876116
10 meter
Z = -16471163
27 Z = -5031288
46
XDOT = 17111
974267 XDOT = 5266
928800
YDOT = -17635
812879 feet/sec YDOT = -5316
784439 meter/sec
ZDOT = 5755
360805 ZDOT = 1779
695932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13270173
08 X = -4044748
75
Y = -6146605
96 feet Y = -1873485
50 meter
Z = -16512596
76 Z = -5033039
49
XDOT = 3465
932844 XDOT = 1056
416331
YDOT = -23268
970286 feet/sec YDOT = -7092
382143 meter/sec
ZDOT = 5850
651747 ZDOT = 1783
278652
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07129
48158962
00020000 00000-0 20000-3 0 9056
2 25544 51
6310 303
8831 0010042 164
7242 195
4228 15
77713504 4664
Satellite: ISS
Catalog Number: 25544
Epoch time: 07129
48158962 = yrday
fracday
Element set: 905
Inclination: 51
6310 deg
RA of node: 303
8831 deg
Eccentricity:
0010042
Arg of perigee: 164
7242 deg
Mean anomaly: 195
4228 deg
Mean motion: 15
77713504 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 466
Checksum: 282
Coasting Arc #7 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2007/130/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4616209
91 A = 6718282
53 meter
Y = 4068130
50 meter E =
0013707
Z = -2684979
89 I = 51
35851
XDOT = -1785
320599 Wp = 153
60072
YDOT = -5426
787306 meter/sec RA = 298
19312 deg
ZDOT = -5175
101710 TA = 57
20011
MA = 57
06815
Ha = 186
803 n
mi
Hp = 176
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15145045
62 X = -4648314
07
Y = 13346884
85 feet Y = 4016330
13 meter
Z = -8808989
14 Z = -2707483
20
XDOT = -5857
351047 XDOT = -1699
365023
YDOT = -17804
420295 feet/sec YDOT = -5446
270808 meter/sec
ZDOT = -16978
680152 ZDOT = -5183
566400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4403983
13 X = -1342334
06
Y = 19662767
76 feet Y = 5993211
61 meter
Z = -8893285
57 Z = -2710673
44
XDOT = -13672
787908 XDOT = -4167
465754
YDOT = -10723
770600 feet/sec YDOT = -3268
605279 meter/sec
ZDOT = -17011
215128 ZDOT = -5185
018371
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07130
49501739
00020000 00000-0 20000-3 0 9064
2 25544 51
6311 298
6493 0009867 168
4139 191
7255 15
77760248 4823
Satellite: ISS
Catalog Number: 25544
Epoch time: 07130
49501739 = yrday
fracday
Element set: 906
Inclination: 51
6311 deg
RA of node: 298
6493 deg
Eccentricity:
0009867
Arg of perigee: 168
4139 deg
Mean anomaly: 191
7255 deg
Mean motion: 15
77760248 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 482
Checksum: 319
Coasting Arc #8 (Orbit 497)
---------------------------------------
Vector Time (GMT): 2007/131/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 918904
16 A = 6715346
75 meter
Y = 5492385
12 meter E =
0015354
Z = 3734893
31 I = 51
33558
XDOT = -5257
272359 Wp = 123
34689
YDOT = 3752
559901 meter/sec RA = 292
95739 deg
ZDOT = -4220
802071 TA = 11
14339
MA = 11
10943
Ha = 186
718 n
mi
Hp = 176
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3014777
42 X = 839275
69
Y = 18019636
21 feet Y = 5502215
41 meter
Z = 12253586
97 Z = 3739164
22
XDOT = -17248
268894 XDOT = -5278
339304
YDOT = 12311
548233 feet/sec YDOT = 3693
652554 meter/sec
ZDOT = -13847
775824 ZDOT = -4246
393010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13170894
39 X = 4014488
61
Y = 12645669
24 feet Y = 3854399
98 meter
Z = 12270336
44 Z = 3739998
55
XDOT = -5424
137004 XDOT = -1653
276959
YDOT = 19192
350385 feet/sec YDOT = 5849
828397 meter/sec
ZDOT = -13943
739583 ZDOT = -4250
051825
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07131
50842282
00020000 00000-0 20000-3 0 9079
2 25544 51
6305 293
4142 0009944 173
0946 187
0357 15
77769376 4983
Satellite: ISS
Catalog Number: 25544
Epoch time: 07131
50842282 = yrday
fracday
Element set: 907
Inclination: 51
6305 deg
RA of node: 293
4142 deg
Eccentricity:
0009944
Arg of perigee: 173
0946 deg
Mean anomaly: 187
0357 deg
Mean motion: 15
77769376 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 498
Checksum: 314
Coasting Arc #9 (Orbit 513)
---------------------------------------
Vector Time (GMT): 2007/132/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4477272
25 A = 6712528
19 meter
Y = -2268981
58 meter E =
0015989
Z = 4456372
36 I = 51
31636
XDOT = 397
788262 Wp = 146
55560
YDOT = 7019
317170 meter/sec RA = 287
81926 deg
ZDOT = 3155
713165 TA = 271
71250
MA = 271
89563
Ha = 186
500 n
mi
Hp = 176
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14689213
43 X = 4480663
12
Y = -7444165
29 feet Y = -2218895
43 meter
Z = 14620644
24 Z = 4478131
30
XDOT = 1305
079600 XDOT = 303
937646
YDOT = 23029
255808 feet/sec YDOT = 7023
240593 meter/sec
ZDOT = 10353
389648 ZDOT = 3157
417947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6962641
29 X = 2122213
06
Y = -14842992
71 feet Y = -4524144
18 meter
Z = 14702347
42 Z = 4481275
49
XDOT = 14037
677572 XDOT = 4278
684124
YDOT = 16907
311923 feet/sec YDOT = 5153
348674 meter/sec
ZDOT = 10360
660277 ZDOT = 3157
929252
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07132
52180511
00020000 00000-0 20000-3 0 9083
2 25544 51
6301 288
1789 0009922 177
0028 183
1198 15
77831197 5148
Satellite: ISS
Catalog Number: 25544
Epoch time: 07132
52180511 = yrday
fracday
Element set: 908
Inclination: 51
6301 deg
RA of node: 288
1789 deg
Eccentricity:
0009922
Arg of perigee: 177
0028 deg
Mean anomaly: 183
1198 deg
Mean motion: 15
77831197 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 514
Checksum: 293
Coasting Arc #10 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2007/133/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 162049
47 A = 6720135
65 meter
Y = -6532542
50 meter E =
0006081
Z = -1582268
32 I = 51
33558
XDOT = 4981
099330 Wp = 125
21420
YDOT = -1261
834565 meter/sec RA = 282
59232 deg
ZDOT = 5731
789780 TA = 217
24415
MA = 217
28634
Ha = 186
451 n
mi
Hp = 176
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 531658
36 X = 242771
75
Y = -21432226
06 feet Y = -6530278
97 meter
Z = -5191169
02 Z = -1581285
26
XDOT = 16342
189402 XDOT = 4966
994722
YDOT = -4139
877182 feet/sec YDOT = -1206
212219 meter/sec
ZDOT = 18805
084580 ZDOT = 5755
954013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13007623
82 X = -3964723
74
Y = -17042738
12 feet Y = -5194626
58 meter
Z = -5188256
96 Z = -1581380
72
XDOT = 8805
355165 XDOT = 2683
872254
YDOT = -12460
953852 feet/sec YDOT = -3798
098734 meter/sec
ZDOT = 18895
971010 ZDOT = 5759
491964
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07133
47183146
00020000 00000-0 20000-3 0 9096
2 25544 51
6310 283
2708 0009962 179
6691 180
4482 15
77851876 5291
Satellite: ISS
Catalog Number: 25544
Epoch time: 07133
47183146 = yrday
fracday
Element set: 909
Inclination: 51
6310 deg
RA of node: 283
2708 deg
Eccentricity:
0009962
Arg of perigee: 179
6691 deg
Mean anomaly: 180
4482 deg
Mean motion: 15
77851876 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 529
Checksum: 319
Coasting Arc #11 (Orbit 544)
---------------------------------------
Vector Time (GMT): 2007/134/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4207516
07 A = 6709047
96 meter
Y = -174402
29 meter E =
0017158
Z = -5234836
39 I = 51
29402
XDOT = 724
713314 Wp = 122
30968
YDOT = -7655
568620 meter/sec RA = 277
42201 deg
ZDOT = -337
289799 TA = 144
52843
MA = 144
41421
Ha = 186
193 n
mi
Hp = 176
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13804186
58 X = -4179822
76
Y = -572185
99 feet Y = -221297
94 meter
Z = -17174660
06 Z = -5255209
66
XDOT = 2377
668352 XDOT = 811
903658
YDOT = -25116
694946 feet/sec YDOT = -7646
976943 meter/sec
ZDOT = -1106
593830 ZDOT = -333
557732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10892651
19 X = -3320080
08
Y = 8342057
22 feet Y = 2542659
04 meter
Z = -17251438
88 Z = -5258238
57
XDOT = -13650
826018 XDOT = -4160
771770
YDOT = -20019
333608 feet/sec YDOT = -6101
892884 meter/sec
ZDOT = -1093
459889 ZDOT = -333
286574
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07134
48517016
00020000 00000-0 20000-3 0 9107
2 25544 51
6314 278
0363 0009872 183
0779 177
0327 15
77899369 5457
Satellite: ISS
Catalog Number: 25544
Epoch time: 07134
48517016 = yrday
fracday
Element set: 910
Inclination: 51
6314 deg
RA of node: 278
0363 deg
Eccentricity:
0009872
Arg of perigee: 183
0779 deg
Mean anomaly: 177
0327 deg
Mean motion: 15
77899369 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 545
Checksum: 316
Coasting Arc #12 (Orbit 560)
---------------------------------------
Vector Time (GMT): 2007/135/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1067782
78 A = 6720532
45 meter
Y = 6546198
86 meter E =
0017947
Z = -1013737
51 I = 51
33057
XDOT = -4667
711962 Wp = 164
64529
YDOT = -1670
219856 meter/sec RA = 272
23858 deg
ZDOT = -5909
703200 TA = 26
51232
MA = 26
42063
Ha = 185
914 n
mi
Hp = 177
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3503224
34 X = -1135979
30
Y = 21477030
40 feet Y = 6533877
10 meter
Z = -3325910
46 Z = -1019089
98
XDOT = -15314
015622 XDOT = -4619
979459
YDOT = -5479
723937 feet/sec YDOT = -1722
149410 meter/sec
ZDOT = -19388
790026 ZDOT = -5932
263686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11402762
68 X = 3475562
07
Y = 18530600
35 feet Y = 5648126
99 meter
Z = -3345287
67 Z = -1019643
68
XDOT = -13737
552001 XDOT = -4187
205850
YDOT = 4961
822677 feet/sec YDOT = 1512
363552 meter/sec
ZDOT = -19473
992366 ZDOT = -5935
672873
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07135
49848534
00020000 00000-0 20000-3 0 9112
2 25544 51
6312 272
7999 0009679 187
8049 172
2967 15
77942780 5619
Satellite: ISS
Catalog Number: 25544
Epoch time: 07135
49848534 = yrday
fracday
Element set: 911
Inclination: 51
6312 deg
RA of node: 272
7999 deg
Eccentricity:
0009679
Arg of perigee: 187
8049 deg
Mean anomaly: 172
2967 deg
Mean motion: 15
77942780 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 561
Checksum: 343
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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